A seal assembly for effecting a seal between two machine components has a housing (15) which defines a channel in which is slidably located an elongate brush seal member (21). A wave spring (28) is located in the channel between the base thereof and the brush seal member to urge the latter outwardly. The brush seal member has a plurality of bristles (24) the free ends of which bear on the second component against which a seal is to be effected, the bristles being disposed between a pair of support plates (22 and 23). On the low-pressure side of the seal, the support plate (23) extends almost to the free tips (26) of the bristles (24) and has a rubbing surface (27) which extends to and is intended to contact the surface against which a seal is to be effected. In the case of a circular seal assembly, a ring may surround the brush seal member and wave spring, whereby the ring, spring and brush seal member are all capable of floating within the channel in the housing.

Patent
   5474305
Priority
Sep 18 1990
Filed
Mar 17 1993
Issued
Dec 12 1995
Expiry
Dec 12 2012
Assg.orig
Entity
Small
126
12
all paid
20. A seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidable mounted in the channel for movement towards and away from said surface, the seal member being in the form of a brush seal member comprising a plurality of closely-packed bristles the free tips of which are adapted to bear on and effect a seal against said surface, retention means to retain the brush seal member in the channel of the housing, and spring means disposed in said channel and arranged to urge said seal member towards said surface of the other component, the spring means allowing the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means.
1. A seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidably mounted in the channel for movement towards and away from said surface, and spring means disposed in said channel and arranged to urge the brush seal member towards said surface of the other component, characterized in that the seal member is in the form of a brush seal member comprising a plurality of closely-packed bristles the free tips of which are adapted to bear on and effect a seal against said surface, in that the spring means allows the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means, and in that the housing is in two relatively separate parts which when fitted together define the channel, and a wall of the housing defining said channel has an in-turned lip which projects transversely across the mouth of the channel.
9. A seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidably mounted in the channel for movement towards and away from said surface, and spring means disposed in said channel and arranged to urge said seal member toward said surface of the other component, characterized in that said seal member is formed in several pieces arranged end-to-end in a relatively movable manner, each said piece being in the form of a brush seal member comprising a plurality of closely-packed bristles the free tips of which are adapted to bear on and effect a seal against said surface, the bristles of one piece overlapping the bristles of the next adjacent piece in the region of a junction between the two pieces, and further characterized in that the spring means allows said pieces of the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means.
8. A seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidably mounted in the channel for movement towards and away from said surface, and spring means disposed in said channel and arranged to urge the brush seal member towards said surface of the other component, characterized in that the seal member is in the form of a brush seal member comprising a plurality of closely-packed bristles the free tips of which are adapted to bear on and effect a seal against said surface, in that the spring means allows the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means, and in that the housing defines an annular channel, the brush seal member is annular and there is provided an endless ring within the channel which ring encircles the brush seal member, the spring means being disposed between and acting on said ring and the brush seal member.
14. A seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidably mounted in the channel for movement towards and away from said surface, and spring means disposed in said channel and arranged to urge said seal member towards said surface of the other component, characterized in that the seal member is in the form of a brush seal member comprising a plurality of closely-packed bristles arranged in two layers disposed immediately side-by-side, the free tips of which bristles are adapted to bear on and effect a seal against said surface, and the bristles of one layer extending at an acute angle to the surface to be sealed and the bristles of the other layer extending at a similar, but oppositely-directed, acute angle to said surface, and further characterized in that the spring means allows the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means.
2. A seal assembly as claimed in claim 1, wherein the brush seal member is formed in several pieces arranged end-to-end in a relatively movable manner.
3. A seal assembly as claimed in claim 2, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal members and on a wall of the housing defining the base of the channel.
4. A seal assembly as claimed in claim 1, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal members and on a wall of the housing defining the base of the channel.
5. A seal assembly as claimed in claim 1, wherein the bristles of the brush seal member are located between a pair of support plates which bear on the outermost bristles of the brush seal member, one of the support plates extending towards the free tips of the bristles to a greater extent than the other support plate.
6. A seal assembly according to claim 5, wherein said one support plate is provided with a rubbing surface on the edge thereof nearer the free tips of the bristles, which rubbing surface extends substantially to the plane of the free tips of the bristles.
7. A seal assembly as claimed in claim 1, wherein two or more brush seal members are provided within a single channel in the housing, each brush seal member being separately spring-urged towards the surface to be sealed of the other machine components.
10. A seal assembly as claimed in claim 9, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the pieces of the seal member and on a wall of the housing defining the base of the channel.
11. A seal assembly as claimed in claim 9, wherein the bristles of each piece of the seal member are located between a pair of support plates which bear on the outermost bristles of the seal member, one of the support plates extending towards the free tips of the bristles to a greater extent than the other support plate.
12. A seal assembly according to claim 11, wherein said one support plate is provided with a rubbing surface on the edge thereof nearer the free tips of the bristles, which rubbing surface extends substantially to the plane of the free tips of the bristles.
13. A seal assembly as claimed in claim 9, wherein each piece of the seal member has two layers of bristles disposed immediately side-by-side, the bristles of one layer extending at an acute angle to the surface to be sealed and the bristles of the other layer extending at a similar, but oppositely-directed, acute angle to said surface.
15. A seal assembly as claimed in claim 14, wherein the brush seal member is formed in several pieces arranged end-to-end in a relatively movable manner.
16. A seal assembly as claimed in claim 15, wherein the bristles of one piece overlap the bristles of the next adjacent piece in the region of a junction between the two pieces.
17. A seal assembly as claimed in claim 16, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal members and on a wall of the housing defining the base of the channel.
18. A seal assembly as claimed in claim 14, wherein the bristles of the brush seal member are located between a pair of support plates which bear on the outermost bristles of the brush seal member, one of the support plates extending towards the free tips of the bristles to a greater extent than the other support plate.
19. A seal assembly according to claim 18, wherein said one support plate is provided with a rubbing surface on the edge thereof nearer the free tips of the bristles, which rubbing surface extends substantially to the plane of the free tips of the bristles.
21. A seal assembly as claimed in claim 20, wherein the brush seal member is formed in several pieces arranged end-to-end in a relatively movable manner.
22. A seal assembly as claimed in claim 21, wherein the bristles of one piece overlap the bristles of the next adjacent piece in the region of a junction between the two pieces.
23. A seal assembly as claimed in claim 22, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal members and on a wall of the housing defining the base of the channel.
24. A seal assembly as claimed in claim 20, wherein the spring means comprises a wave spring extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal members and on a wall of the housing defining the base of the channel.
25. A seal assembly as claimed In claim 20, wherein the bristles of the brush seal member are located between a pair of support plates which bear on the outermost bristles of the brush seal member, one of the support plates extending towards the free tips of the bristles to a greater extent than the other support plate.
26. A seal assembly according to claim 25, wherein said one support plate is provided with a rubbing surface on the edge thereof nearer the free tips of the bristles, which rubbing surface extends substantially to the plane of the free tips of the bristles.
27. A seal assembly according to claim 20, wherein the housing is in two relatively separate parts which when fitted together define the channel, and a wall of the housing defining said channel having an in-turned lip which projects transversely across the mouth of the channel.
28. A seal assembly as claimed in claim 20, wherein the housing defines an annular channel, the brush seal member is annular and there is provided an endless ring within the channel which ring encircles the brush seal member, the spring means being disposed between and acting on said ring and the brush seal member.

1. Field of the Invention

This invention relates to a seal assembly, and in particular to a seal assembly suitable for effecting a seal between two machine components.

2. Description of the Related Art

It is frequently necessary to effect a fluid-tight seal between two machine components which may move one with respect to the other. For example, it may be necessary to effect a seal between a housing having a bore and a shaft which extends through the bore; or to effect a seal between the two components of a ball joint. There have been innumerable proposals for seal devices adapted to effect such seals between two relatively-movable machine components, and it is necessary for a machine designer to select the most appropriate type of seal device, having regard to the operating conditions which may be expected to be encountered.

In the case of machine components which are to be sealed one to the other in the presence of pressurised hot gases, it is known to use a brush seal assembly, on account of the unsatisfactory performance of a simpler seal having for example a synthetic elastomeric annular sealing member clamped to one of the machine components and bearing on the other component. In the case of a brush seal, a plurality of fine bristles (such as of bronze, chrome-nickel alloy or other alloy wires) is held in a carrier mounted on one of the machine components such that the tips of the bristles wipe against the other machine component, so as thereby to effect a seal between the two components.

It is a characteristic of the known designs of brush seal that they must be manufactured to very close tolerances, in order to achieve an effective seal. If the bristles are too short, there will be a gas leakage path between the tips of the bristles and the other machine component against which the seal is to be effected; but on the other hand, if the bristles are too long there will be excessive friction between the bristles and the other machine component, leading to rapid wear of the other machine component. The flexing of the bristles moreover may destroy the effectiveness of the seal, giving a gas leakage path between the bristles.

In addition to the brush seal being manufactured to close tolerances, it is apparent that the machine components also must run true, within fine limits. Whilst this is normally not a problem where for example a shaft is to be sealed to a housing through which the shaft extends, it can be a problem in the case of relatively movable fabricated machine components, which may not be circular. For example, if a seal is to be effected between an adjustable outlet nozzle of a jet engine and the main housing of that jet engine, it may be impractical to manufacture the nozzle and/or the housing to tolerances closer than 1 mm, especially if the nozzle diameter is relatively large. In such a case, one function of a seal device disposed between the components is to take up the manufacturing tolerances, whilst still maintaining a seal between the two components.

It is a principal object of the present invention to provide a brush seal suitable for use between two machine components to effect a seal therebetween, even when the clearance between the two machine components cannot be guaranteed to lie within a closely-controlled tolerance range.

Accordingly, this invention provides a seal assembly for effecting a seal between two machine components the clearance between which may vary slightly, which assembly comprises a housing attached to or forming a part of one of the machine components and defining a channel facing the surface to be sealed of the other component, a seal member slidably mounted in the channel for movement towards and away from said surface, and spring means disposed in said channel and arranged to urge the seal member towards said surface of the other component, characterised in that the seal member is in the form of a brush seal member comprising a plurality of closely-packed bristles the free tips of which are adapted to bear on and effect a seal against said surface, and in that the spring means allows the brush seal member to accommodate dynamically minor variations in the clearance between the two components by movement of the seal member against the spring bias provided by the spring means.

It will be appreciated that in the seal assembly of this invention, at least small changes in the clearance between the two machine components sealed together by the brush seal member may be accommodated by the brush seal member itself slidably moving within its housing, rather than by the bristles of the brush seal member deflecting and so giving a gas leakage path. Thus, an enhanced sealing effect may be obtained even when the two machine components are not manufactured to very close tolerances. Also, the seal assembly may be used to obtain an effective seal when the gap between the two surfaces to be sealed varies due to thermal, dynamic or other stresses which may cause surface distortions.

A further advantage of the seal assembly of this invention is that non-circular machine components may be sealed one to the other. To facilitate this, it is preferred for the brush seal member either to be flexible along its length or to be formed in several separate pieces arranged end-to-end in a relatively movable manner, whereby a change in the clearance between the two machine components at one location will not significantly affect the sealing effect obtained at a location spaced therefrom. In the case of a multi-piece seal, the bristles of one piece may overlap those of another piece, to maintain the sealing effect in the region of a junction between two pieces.

Preferably, the spring means comprises a so-called wave spring, extending along the length of the channel in which the brush seal member is slidably mounted, the wave spring bearing at a plurality of spaced and alternate points on the brush seal member and a wall of the housing defining the base of the channel. Such a wave spring may be formed from a single blade of a spring steel material, though two or more such blades may be used in parallel if required, to give a greater spring force. An alternative arrangement would be for there to be mounted within the channel a plurality of helical springs each disposed with its axis substantially perpendicular to a tangent to the length of the brush seal member at the point where the spring contacts that member. In such an arrangement, suitable location means may be provided for each helical spring.

For a brush seal assembly of this invention intended for use in an environment where high temperatures are not encountered, it would be possible to use spring means in the form of an elongated strip of elastomeric or other resilient material located in the channel between a wall of the housing defining the base of the channel and the brush seal member itself.

Preferably, the brush seal member has the bristles thereof located between a pair of support plates which bear on the outermost bristles of the brush seal member, one of the support plates extending towards the free tips of the bristles to a greater extent than the other support plate. Said one support plate may thus serve to resist flexing of the bristles in the event that the brush seal member is subjected to a large pressure differential, with the low pressure side of the seal assembly being that on which the said one support plate is located.

In order to give support as close as possible to the free tips of the bristles, said one support plate may have a rubbing surface provided on the edge thereof nearer the free tips of the bristles, which rubbing surface extends substantially to the plane of the free tips of the bristles, and is intended to rub on the sealing surface of said other component. Such a rubbing surface should be adapted to resist galling and pick-up from the sealing surface of the other component; for example, such a rubbing surface may be a cobalt-based alloy applied by a plasma spray system. In this way, the support plate itself may also perform a sealing function.

Though the channel in the housing, and so also the brush seal member, may be endless, for example when a seal is to be effected between two circular or spherical components, the seal assembly of this invention may also be used in circumstances where an endless seal is not practical. For example, the seal assembly may be used to effect a seal between two flat or curved plates which are to move relatively to some limited extent. In such a case, it is preferred for there to be two layers of bristles disposed immediately side by side in the seal member, with the bristles of one layer extending at an acute angle to the surface to be sealed and the bristles of the other layer extending at a similar, but oppositely-directed, acute angle to said surface. In such a case, the relative movement between the machine components should be in a direction substantially normal to the length of the seal member.

The sealing effect obtained by a seal assembly of this invention as described above may be improved by providing two or more brush seal members within a single channel in a housing, each brush seal member being separately spring-urged towards the surface to be sealed of the other machine component. Alternatively, said housing may have two or more channels, each accommodating a brush seal member spring-urged by its own spring means.

Means may be provided to retain the brush seal member in the channel of the housing, should the other component move away from the housing by more then some pre-determined extent. To this end, the housing may define a lip projecting transversely across the mouth of the channel, engageable by a part of the brush seal member. To permit changing of the seal member, the housing may be in at least two relatively separable parts.

The preferred form of wave spring allows limited movement of the brush seal member before the spring force exerted on the brush seal member rises significantly. If the seal assembly is configured to effect a seal between a housing and a rotatable shaft, significant excursions of the shaft can be accommodated without the seal member being subjected to high spring forces by providing an endless ring within the channel in the housing which ring encircles the brush seal member and the spring means being disposed between and acting on the ring and the brush seal member. In this way, the brush seal member, spring means and ring may move together within the channel to accommodate shaft excursions, the seal member moving against the force of the spring means to accommodate shaft irregularities.

This invention extends to a seal assembly adapted to effect a seal between two machine components the clearance between which may vary slightly, which seal assembly comprises a housing defining an elongate channel, a seal member slidingly received in said channel for movement into and out of the channel in the direction normal to the length of the channel, and spring means located in the channel to urge the seal member out of the housing, characterised in that the seal member takes the form of an elongate brush seal member and in that minor variations in the clearance between the two components is accommodated dynamically by movement of the brush seal member against the spring bias provided by the spring means.

By way of example only, certain specific embodiments of seal assembly arranged in accordance with the present invention will now be described in detail, reference being made to the accompanying drawings, in which:

FIG. 1 is a detailed view of a part of an arcuate seal assembly, with part of the housing cut away for clarity;

FIG. 2 is a sectional view on the assembly of FIG. 1, taken on line II--II but with the housing complete;

FIG. 3 is a view similar to that of FIG. 1, but on a second embodiment of seal assembly;

FIG. 4 is a sectional view taken on line IV--IV shown on FIG. 3, but with the housing complete.

FIG. 5 is a view on a third embodiment of seal assembly, similar to that of FIG. 3;

FIG. 6 is an exploded view showing the junction between two seal elements used in the embodiment of FIG. 5;

FIG. 7 is a view similar to that of FIG. 2, but of yet another embodiment of seal assembly of this invention;

FIGS. 8 and 9 are views similar to those of FIGS. 1 and 2, but on a further embodiment of seal assembly of this invention; and

FIG. 10 is a sectional view similar to FIG. 2 of still another embodiment of the seal assembly of this invention.

Referring initially to FIGS. 1 and 2, the seal assembly there illustrated is intended to effect a seal between two machine components 10 and 11, component 11 being arranged to move at a relatively slow speed with respect to component 10. The sealing surface 12 of component 11 represents an unmachined surface with an uneven contour, and which could be round, spherical, linear, or of some other form. Such a large unmachined surface may typically have an accuracy deviating from a true profile by perhaps 2.5 mm (0.100") and a brush seal assembly of a conventional design cannot be used to effect an adequate seal thereagainst.

An embodiment of brush seal assembly of this invention which is adapted to effect the required seal comprises a housing 15 having a mounting flange 16 provided with bolt-holes 17, side walls 18 and 19 and base wall 20 of the housing 15 defining an elongate channel in which is located a brush seal member 21. The brush seal member comprises a pair of support plates 22 and 23 between which are clamped a layer of bristles 24, the support plates 22 and 23 and bristles 24 being welded together at 25. As shown in FIG. 1, the bristles 24 are disposed to lie at an acute angle to the plane of the surface 12 against which a seal is to be effected. The support plate 23 extends almost to the free tips 26 of the bristles 24, and the support plate 23 has a rubbing surface 27 provided on the end of that plate adjacent the free tips 26, which rubbing surface extends to and is intended to contact the surface 12.

Also located in the channel defined by the housing 15 is a wave spring member 28, bearing at spaced and alternate locations on the base wall 20 of the housing 15 and on the brush seal member 21, as best seen in FIG. 1. The wave spring member 28 thus urges the brush seal member 21 towards the surface 12 of component 11, against which a seal is to be effected.

The configuration is such that the free tips of the bristles 24 project just beyond the rubbing surface 27. When the seal assembly is in use, the spring 28 urges the seal member 21 towards the surface 12 until the rubbing surface makes contact therewith. In this condition, the bristles are flexed very slightly, in the plane of the bristle layer. Should the spacing between the components 10 and 11 vary within a predefined limit, on relative movement between the components, the brush seal member 21 will move as appropriate against the bias provided by the wave spring member 28, so that the rubbing surface 27 maintains contact with the moving surface 12. If however there is a localised surface variation, where the surface 12 locally moves clear of the rubbing surface 27, the bristles 24 will tend to spring across the resultant gap, by virtue of the flexing of the bristles in their own plane.

The brush seal member 21 may be endless, or could be of some predefined length. Moreover, the seal member could be formed in one piece, or in a plurality of sections linked together.

Referring now to FIGS. 3 and 4, there is illustrated a second embodiment of seal assembly of this invention, generally similar to that of FIGS. 1 and 2, and like reference characters will be used to indicates like parts: those parts will not be described again here.

The seal assembly of FIGS. 3 and 4 differs from that shown in FIGS. 1 and 2 in that the seal assembly is essentially linear, rather than arcuate. Moreover, in this alternative form of seal assembly, the bristles 24 are provided in two layers 30 and 31, the bristles of one layer lying at a substantially equal but opposite acute angle to the surface to be sealed as compared to the bristles of the other layer. This arrangement allows for the manufacture of a predefined length of brush seal member, whilst still obtaining a sealing effect right to the ends of that member, defined by end plates 32.

When either seal member of this invention as described above is employed, side A of the seal assembly should be subjected to a higher pressure than the opposed side of the seal, so that the bristles 24 will be supported by the relatively long support plate 23 and flexing of the bristles 24 under the pressure difference across the seal will be avoided.

FIGS. 5 and 6 show how a seal assembly similar to that of FIGS. 3 and 4 may be assembled from a plurality of individual seal elements; like parts with those of FIG. 3 are given like reference characters. In this embodiment, the linear housing 15 has a linear seal member consisting of a plurality of seal elements 35, each having bristles 24 in two layers 30 and 31 of oppositely inclined bristles. FIG. 6 shows the bristle arrangement at a junction 36 between two elements 35, and it can be seen that the overlapping of the bristles is continued at the junction, so giving continuity of the sealing effect. The ends of the seal member (not shown) may be arranged as shown in FIG. 3.

A particular advantage of the arrangement illustrated in FIGS. 5 and 6 is that small movements are possible between the seal elements 35, so permitting an enhanced sealing effect where a long seal is required and the gap between the surfaces to be sealed is not constant.

In an alternative but similar arrangement, each seal element may be as illustrated in FIG. 3; relative movements between the elements would still be possible, though the sealing effect at the junctions between elements may not be quite so good.

In the seal assembly of FIG. 1, the seal member may drop out of the channel in the housing 15 in the event that the component 11 moves away from the housing by too great an extent. The seal assembly of FIG. 7 has a modified housing to overcome this; here the housing is in two parts 40 and 41 held together by the mounting bolts (not shown) which pass through the holes 17. Housing part 40 defines side wall 19 and a flange 42 extending at right angles thereto; and housing part 41 defines side wall 18 and bears on the flange 42. The side wall 18 has an in-turned lip 43 at its free end, against which the plate 22 of the seal member 21 will bear if the component 11 moves away from the housing 15.

The seal member is then shown as having two rows of bristles 44 and 45, but in other respects the arrangement corresponds to that illustrated in FIGS. 1 and 2; it will not be described further here.

FIGS. 8 and 9 show yet another arrangement of seal assembly, generally similar to that of FIGS. 1 and 2, but intended for use on a circular shaft 50. In this assembly, a housing is constructed from housing parts 51 and 52, held together by bolt 53 to define a channel 54 in which is slidably mounted a multi-element brush seal member 55, having one row of bristles 56. Each element is welded from a pair of support plates 57 and 58 with the bristles 56 therebetween. Housing part 52 has an in-turned lip 59 to retain the seal member in the housing, as described above with reference to FIG. 7.

Also located in the housing 51 is a continuous ring 60 surrounding the brush seal member 55, with a wave-spring 61 positioned between the ring 60 and seal member 55. The whole of the seal member together with the ring 60 and spring 61 may float in the housing, for example to accommodate excursions of the shaft 50 with respect to the housing, whilst the multi-element seal member urged by spring 61 may accommodate any non-circularity or other variations in the shaft.

FIG. 10 shows still another arrangement of the seal assembly, generally similar to that of FIG. 2, but illustrating two brush seal members provided within a single channel in housing 15. One brush seal member comprises a layer of bristles 24 clamped between a pair of support plates 22 and 23 welded together at 25, while the second brush seal member includes a layer of bristles 24' clamped between a pair of support plates 22' and 23' welded together at 25'. Each brush seal member is separately spring urged by a wave spring member 28, 28', respectively, towards the surface 12 to be sealed so that the free tips 26, 26' of the bristles 24, 24' respectively effect the desired seal. In all other respects, the structure and components illustrated in FIG. 10 is identical to that previously described herein with respect to FIG. 2.

Flower, Ralph F. J.

Patent Priority Assignee Title
10006306, Dec 29 2012 RTX CORPORATION Turbine exhaust case architecture
10053998, Dec 29 2012 RTX CORPORATION Multi-purpose gas turbine seal support and assembly
10054009, Dec 31 2012 RTX CORPORATION Turbine exhaust case multi-piece frame
10060279, Dec 29 2012 RTX CORPORATION Seal support disk and assembly
10087843, Dec 29 2012 RTX CORPORATION Mount with deflectable tabs
10094389, Dec 29 2012 RTX CORPORATION Flow diverter to redirect secondary flow
10138742, Dec 29 2012 RTX CORPORATION Multi-ply finger seal
10208674, Mar 13 2013 RTX CORPORATION Multi-axial brush seal
10240481, Dec 29 2012 RTX CORPORATION Angled cut to direct radiative heat load
10240532, Dec 29 2012 RTX CORPORATION Frame junction cooling holes
10294819, Dec 29 2012 RTX CORPORATION Multi-piece heat shield
10329956, Dec 29 2012 RTX CORPORATION Multi-function boss for a turbine exhaust case
10329957, Dec 31 2012 RTX CORPORATION Turbine exhaust case multi-piece framed
10330011, Mar 11 2013 RTX CORPORATION Bench aft sub-assembly for turbine exhaust case fairing
10352183, Apr 25 2016 RTX CORPORATION High temperature seal and method
10364748, Aug 19 2016 RTX CORPORATION Finger seal flow metering
10378370, Dec 29 2012 RTX CORPORATION Mechanical linkage for segmented heat shield
10472987, Dec 29 2012 RTX CORPORATION Heat shield for a casing
10487687, Sep 15 2016 RTX CORPORATION Gas turbine engine having a seal damper assembly
10633997, Aug 20 2010 MITSUBISHI HITACHI POWER SYSTEMS AMERICAS, INC Inter stage seal housing having a replaceable wear strip
10900365, Nov 29 2012 SAFRAN AIRCRAFT ENGINES Assembly forming a gasket for a turbomachine, comprising a brush seal
10941674, Dec 29 2012 RTX CORPORATION Multi-piece heat shield
11428323, Apr 16 2019 RTX CORPORATION Floating brush seal assembly
11867224, Jan 27 2021 Black & Decker Inc Locking mechanism for two telescoping poles of a power tool
5749584, Nov 19 1992 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines
5752805, Jul 28 1995 MTU Aero Engines GmbH Brush seal for turbo-engines
5799952, Dec 09 1995 Rolls-Royce plc Brush seal
5997004, Oct 22 1996 Flowserve Corporation; FLOWSERVE INTERNATIONAL, INC ; FLOWSERVE HOLDINGS, INC ; Flowserve Management Company Hybrid floating brush seal
6010132, Nov 19 1992 General Electric Co. Hybrid labyrinth and cloth-brush seals for turbine applications
6027121, Oct 23 1997 General Electric Company Combined brush/labyrinth seal for rotary machines
6042119, Nov 19 1992 General Electric Co. Woven seals and hybrid cloth-brush seals for turbine applications
6045134, Feb 04 1998 General Electric Company Combined labyrinth and brush seals for rotary machines
6077038, Jul 28 1995 MTU Aero Engines GmbH Brush seal for turbo engines
6079945, Nov 10 1997 Geneal Electric Company Brush seal for high-pressure rotor applications
6105967, Feb 04 1998 General Electric Company Combined labyrinth and brush seals for rotary machines
6131910, Nov 19 1992 General Electric Co. Brush seals and combined labyrinth and brush seals for rotary machines
6131911, Nov 19 1992 General Electric Company Brush seals and combined labyrinth and brush seals for rotary machines
6139018, Mar 25 1998 General Electric Company Positive pressure-actuated brush seal
6161836, Aug 25 1998 General Electric Company Brush seal and rotary machine containing such brush seal
6168162, Aug 05 1998 General Electric Company Self-centering brush seal
6168377, Jan 27 1999 General Electric Company Method and apparatus for eliminating thermal bowing of steam turbine rotors
6170831, Dec 23 1998 United Technologies Corporation Axial brush seal for gas turbine engines
6173958, Nov 19 1992 General Electric Co. Hybrid labyrinth and cloth-brush seals for turbine applications
6173962, Dec 09 1995 Rolls Royce PLC Brush seal
6227545, Oct 28 1997 Voith Sulzer Papiertechnik Patent GmbH Heatable and/or coolable cylinder
6231047, May 29 1998 Eaton Corporation Brush seal
6244599, Apr 28 1999 Flowserve Management Company Floating brush seal
6250640, Aug 17 1998 General Electric Company Brush seals for steam turbine applications
6257586, Nov 19 1992 General Electric Co. Combined brush seal and labyrinth seal segment for rotary machines
6290232, Nov 16 1999 General Electric Company Rub-tolerant brush seal for turbine rotors and methods of installation
6331006, Jan 25 2000 General Electric Company Brush seal mounting in supporting groove using flat spring with bifurcated end
6357672, Jul 06 1995 United Technologies Corporation Sealing means for a multi-axis nozzle
6378873, Jun 02 2000 General Electric Company Low flow fluid film seal for hydrogen cooled generators
6382632, Feb 21 2001 General Electric Company Repositionable brush seal for turbomachinery
6402157, Aug 20 2001 General Electric Company Brush seal and method of using brush seal
6416057, Apr 16 1999 Flowserve Management Company Brush seal
6435513, Nov 19 1992 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines
6464230, Oct 19 2000 General Electric Company Flexible magnetic rubber brush seal for generators
6502824, Dec 15 2000 General Electric Company Brush seal for a bearing cavity
6536773, Nov 06 2000 Advanced Components & Materials, Inc.; ADVANCED COMPONENTS & MATERIALS, INC A RHODE ISLAND CORPORATION Compliant brush shroud assembly for gas turbine engine compressors
6540231, Feb 29 2000 General Electric Company Surface following brush seal
6550777, Jun 19 2001 General Electric Company Split packing ring segment for a brush seal insert in a rotary machine
6589012, Sep 24 2001 General Electric Company Method and apparatus for eliminating thermal bowing using brush seals in the diaphragm packing area of steam turbines
6595946, Feb 25 2000 Tyco Healthcare Group LP Valve assembly
6612581, Dec 04 2001 General Electric Company Brush seal coil for rotary machinery and method of retrofitting
6669203, Jul 11 2002 General Electric Company Brush seal placement between rotating and stationary components with reversely bent leaf spring
6679500, Sep 25 2002 GENERAL ELECTRIC TECHNOLOGY GMBH Coal pulverizer brush seal assembly
6685190, Oct 17 2000 General Electric Company Ventilated trickle seal
6739592, Mar 27 2001 Eagle Engineering Aerospace Co., Ltd. Brush seal device
6811154, Feb 08 2003 The United States of America as represented by the Administrator of the National Aeronautics and Space Administration Noncontacting finger seal
6821086, Jun 03 2003 General Electric Company Turbomachine seal assembly and method therefor
6880829, Nov 06 2000 ADVANCED COMPONENTS & MATERIALS, INC Compliant brush shroud assembly for gas turbine engine compressors
6910858, Dec 26 2002 RAYTHEON TECHNOLOGIES CORPORATION Seal
6913265, Aug 09 2000 ADVANCED COMPONENTS & MATERIALS, INC Brush seal assembly, method of manufacture and use
6923783, Feb 25 2000 Tyco Healthcare Group LP Valve assembly
7059827, May 31 1996 Watson Cogeneration Company Turbine power plant having minimal-contact brush seal augmented labyrinth seal
7093835, Aug 27 2002 RTX CORPORATION Floating brush seal assembly
7270333, Nov 27 2002 RAYTHEON TECHNOLOGIES CORPORATION Brush seal with adjustable clearance
7364165, May 21 2003 MITSUBISHI HEAVY INDUSTRIES, INC Shaft seal mechanism
7434813, Oct 28 2004 Rolls-Royce plc Large radial movement compliant seal
7438526, Oct 28 2004 Rolls-Royce plc Large radial movement compliant seal
7445212, Apr 13 2000 MTU Aero Engines GmbH Brush seal
7461847, Dec 12 2005 EATON INTELLIGENT POWER LIMITED Self centering, floating brush seal assembly
7516962, May 08 2003 MTU Aero Engines GmbH Spoke-centered brush seal arrangement for use in a gas turbine
7543822, Jul 12 2004 A W CHESTERTON COMPANY Composite rotary seal assembly
7559918, Feb 25 2000 Tyco Healthcare Group LP Valve assembly
7637719, Aug 11 2004 MTU Aero Engines GmbH Sealing arrangement
7735833, Nov 14 2006 AKRON, UNIVERSITY OF, THE Double padded finger seal
7850655, Feb 25 2000 Covidien LP Valve assembly
7931276, Mar 20 2002 RTX CORPORATION Brush seal
7967297, Mar 13 2007 EATON INTELLIGENT POWER LIMITED Thermally-activated control gap brush seal
8043012, Sep 30 2009 GE INFRASTRUCTURE TECHNOLOGY LLC Seal arrangement and a brush seal for a wind turbine
8152774, Feb 25 2000 Covidien LP Valve assembly
8169766, Mar 17 2003 Illinois Tool Works, Inc. Shaft current control brush ring assembly
8181965, Jun 27 2002 RAYTHEON TECHNOLOGIES CORPORATION Replaceable brush seal elements
8199453, Mar 17 2003 Illinois Tool Works Inc. Shaft current control brush ring assembly
8328198, Oct 06 2010 GE INFRASTRUCTURE TECHNOLOGY LLC Brush seal
8432659, Mar 17 2003 Illinois Tool Works Inc. Shaft current control brush ring assembly
8469656, Jan 15 2008 SIEMENS ENERGY, INC Airfoil seal system for gas turbine engine
8505923, Aug 31 2009 OSBORN, LLC Brush seal with stress and deflection accommodating membrane
8534673, Aug 20 2010 MITSUBISHI POWER, LTD Inter stage seal housing having a replaceable wear strip
8657298, Aug 15 2011 GE INFRASTRUCTURE TECHNOLOGY LLC Brush seal with backing plate tooth
8727354, Jan 15 2008 RTX CORPORATION Brush seal assembly and method of manufacturing same
8919780, Oct 06 2010 GE INFRASTRUCTURE TECHNOLOGY LLC Brush seal
9074487, Aug 17 2011 GE INFRASTRUCTURE TECHNOLOGY LLC Self-lubricating brush seal assembly and method of reducing leakage
9206742, Dec 29 2012 RTX CORPORATION Passages to facilitate a secondary flow between components
9297312, Dec 29 2012 RTX CORPORATION Circumferentially retained fairing
9347330, Dec 29 2012 RTX CORPORATION Finger seal
9470101, Dec 05 2011 NUOVO PIGNONE TECNOLOGIE S R L Turbomachine
9541006, Dec 29 2012 United Technologies Corporation Inter-module flow discourager
9562478, Dec 29 2012 United Technologies Corporation Inter-module finger seal
9631517, Dec 29 2012 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
9714711, Jun 28 2013 Rolls-Royce plc Leaf seal
9771818, Dec 29 2012 RTX CORPORATION Seals for a circumferential stop ring in a turbine exhaust case
9784371, Jun 28 2013 Rolls-Royce plc Brush seal
9828867, Dec 29 2012 RTX CORPORATION Bumper for seals in a turbine exhaust case
9845695, Dec 29 2012 RTX CORPORATION Gas turbine seal assembly and seal support
9850774, Dec 29 2012 RTX CORPORATION Flow diverter element and assembly
9850780, Dec 29 2012 RTX CORPORATION Plate for directing flow and film cooling of components
9863261, Dec 29 2012 RTX CORPORATION Component retention with probe
9890663, Dec 31 2012 RTX CORPORATION Turbine exhaust case multi-piece frame
9903216, Dec 29 2012 RTX CORPORATION Gas turbine seal assembly and seal support
9903224, Dec 29 2012 RTX CORPORATION Scupper channelling in gas turbine modules
9903476, Dec 25 2012 SHOJI, SUSUMU; SANWA TECHNO CO , LTD Cylindrical shaft-sealing material obtained from pile weave or knit
9982561, Dec 29 2012 RTX CORPORATION Heat shield for cooling a strut
9982564, Dec 29 2012 RTX CORPORATION Turbine frame assembly and method of designing turbine frame assembly
Patent Priority Assignee Title
4358120, May 31 1980 Rolls Royce Limited; Rolls-Royce Limited Seals
4989886, Dec 30 1988 Textron Inc Braided filamentary sealing element
5042823, Dec 21 1989 Allied-Signal Inc. Laminated finger seal
5066025, Jun 18 1990 UNITED TECHNOLOGIES CORPORATION, A CORP OF DE Brush seal assembly
5090710, May 29 1987 Cross Manufacturing Company (1938) Limited Brush seals
5176389, Feb 21 1991 United Technologies Segmented brush seal
5201530, Oct 18 1991 United Technologies Corporation Multi-layered brush seal
5265412, Jul 28 1992 General Electric Company Self-accommodating brush seal for gas turbine combustor
EP453315,
GB2258277,
WO2014951,
WO3003299,
//
Executed onAssignorAssigneeConveyanceFrameReelDoc
Mar 12 1993FLOWER, RALPH FRANKLYN JOHNCROSS MANUFACTURING COMPANY 1938 LIMITEDASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0071180312 pdf
Mar 17 1993Cross Manufacturing Company (1938) Limited(assignment on the face of the patent)
Date Maintenance Fee Events
May 27 1999M283: Payment of Maintenance Fee, 4th Yr, Small Entity.
Jun 02 2003M2552: Payment of Maintenance Fee, 8th Yr, Small Entity.
May 22 2007M2553: Payment of Maintenance Fee, 12th Yr, Small Entity.


Date Maintenance Schedule
Dec 12 19984 years fee payment window open
Jun 12 19996 months grace period start (w surcharge)
Dec 12 1999patent expiry (for year 4)
Dec 12 20012 years to revive unintentionally abandoned end. (for year 4)
Dec 12 20028 years fee payment window open
Jun 12 20036 months grace period start (w surcharge)
Dec 12 2003patent expiry (for year 8)
Dec 12 20052 years to revive unintentionally abandoned end. (for year 8)
Dec 12 200612 years fee payment window open
Jun 12 20076 months grace period start (w surcharge)
Dec 12 2007patent expiry (for year 12)
Dec 12 20092 years to revive unintentionally abandoned end. (for year 12)